EP2636516A1 - System zur Platzierung von kleinem flachem Verbundwerkstoff - Google Patents

System zur Platzierung von kleinem flachem Verbundwerkstoff Download PDF

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Publication number
EP2636516A1
EP2636516A1 EP13158291.8A EP13158291A EP2636516A1 EP 2636516 A1 EP2636516 A1 EP 2636516A1 EP 13158291 A EP13158291 A EP 13158291A EP 2636516 A1 EP2636516 A1 EP 2636516A1
Authority
EP
European Patent Office
Prior art keywords
tool
axis
composite
head
composite placement
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP13158291.8A
Other languages
English (en)
French (fr)
Other versions
EP2636516B1 (de
Inventor
Randall A. Kappesser
Richard A. Curless
Michael A. Noel
Daniel D. Janka
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Fives Machining Systems Inc
Original Assignee
MAG IAS LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by MAG IAS LLC filed Critical MAG IAS LLC
Publication of EP2636516A1 publication Critical patent/EP2636516A1/de
Application granted granted Critical
Publication of EP2636516B1 publication Critical patent/EP2636516B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/0046—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by constructional aspects of the apparatus
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/30—Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/12—Surface bonding means and/or assembly means with cutting, punching, piercing, severing or tearing
    • Y10T156/1348—Work traversing type
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
    • Y10T156/17—Surface bonding means and/or assemblymeans with work feeding or handling means
    • Y10T156/1788—Work traversing type and/or means applying work to wall or static structure

Definitions

  • the device relates to a substantially stationary fiber placement head and material delivery system for producing small flat laminates in which the material is not being manipulated by the machine as it is being dispensed and relative motion between the head and the tool is achieved by movement of the tool relative to the stationary head.
  • Composite placement machines for forming high strength low weight articles from high strength fiber or tape and a resin binder are well known in the art.
  • Such machines normally comprise a composites placement head supported by an overhead gantry mechanism, or mounted on the end of a manipulator such as a robot arm. The head is maneuvered on the end of its support to apply composite material to the tool as required.
  • the tool may also be non-stationary during material application as in the case of a cylindrical form or tool that is rotated around its center axis.
  • Such machines are large and expensive, and the use of a gantry or robot based machine to fabricate a small flat part is not an efficient use of resources.
  • Large composite layup machines are used to produce aircraft skins made of composite material, for example, tape laying machines for parts like wings and stabilizers, and fiber placement machines for fuselages, nacelles, and similar contoured parts.
  • tape laying machines for parts like wings and stabilizers
  • fiber placement machines for fuselages, nacelles, and similar contoured parts.
  • a common method for manufacturing these small composite parts is to use a large machine to create a flat laminate that is cut to size and draped over a tool to form the small part's final shape.
  • a flat laminate is made much larger than the single small part and multiple flat laminates are cut out from the single large laminate, creating a large amount of waste material for the portions that are not useable.
  • FIG 1 is a perspective view of a composite machine generally designated by the reference numeral 10 for producing small flat parts.
  • the machine comprises a creel 12 that is mounted on a base 14 that rests on the floor.
  • the creel 12 holds a number of spools 16 of material that will be used to make a part. Although it is anticipated that the material will comprise fiber in the form of slit tape or tow, tape could also be used.
  • the creel 12 holds twelve spools of fiber material on one side, and the creel may hold twelve additional spools of fiber material on the opposite side. Twenty four spools will allow the head to lay down twenty four lanes of material at a time.
  • the creel may also be designed to hold twelve or sixteen spools, or more than twenty four spools.
  • the composite material may comprise slit tape having a width of one-half inch, or other widths as desired. Positioning the spools 16 on both sides of the creel 12 reduces the footprint of the creel compared to a creel on which an equal number of spools are all supported on one side of the creel.
  • Fiber material 15 from the spools 16 is threaded upwards to first redirect rollers 18 mounted on top of the creel that direct the fiber to the center of the creel, and to second redirect rollers 20 that direct the fiber to a Z-axis redirect roller 22 mounted on the top of a fiber placement head 24.
  • Guides 26 may be positioned along the fiber path as required to guide or support the fiber 15 between the redirect rollers on the creel and the Z-axis redirect roller 22.
  • the creel 12 has a front wall 30 and a vertical slide 34 is mounted on the front wall 30.
  • a bracket 32 is coupled to the vertical slide 34, and the head 24 is mounted on the bracket 32.
  • the vertical slide 34 driven by a linear actuator 36 that allows the head 24 to raise or lower a small amount in the Z-axis relative to the creel 12.
  • the amount of vertical movement allowed by the vertical slide 34 may be 10 inches or less, and preferably is 2 inches or less.
  • Motion of the head 24 in the Z-axis can be performed with a relatively small actuator 36 since the moving mass of the head 24 does not include a heavy wrist mechanism. There is only a small spool rewind requirement to accommodate the short vertical axis movement of the head in the Z-axis relative to the tool.
  • a tool 40 that receives fiber composite material may be positioned on a rotary C-axis table 42 that is next to the creel and beneath the head 24.
  • Motion of the head 24 in the Z-axis is only performed at the beginning or end of a course in order to lower or raise the compaction roller or shoe 46 at the lower end of the head 24 onto or off of the layup surface or laminate as required.
  • Motion of the head in the Z-axis is also performed in order to initially position a tool under the head for a layup operation, and to remove a complete layup part from the C-axis table.
  • Figure 1 shows the roller or shoe 46 in a raised position in solid, and in a lowered position in phantom.
  • the head 24 contains an internal compactor slide (not shown) that is used to raise and lower the compaction roller or shoe 46 relative to the tool 40.
  • the mounting of the head on the creel 12 does not allow movement of the head 24 in the X-axis or the Y-axis.
  • the bracket 32 may be provided with a horizontal Y-axis pivot 44 that allows the head 24 to swivel about the pivot 44 for cleaning or servicing purposes. Pivoting movement of the head 24 about the Y-axis is not performed while the head is applying composite material to a tool 40.
  • composite material is always applied to the tool 40 in a direction that is at right angles to the width dimension of the compaction roller or shoe 46.
  • Figure 2 shows the possible motions of the X, Y, and Z-axis tables.
  • the rotary motion of the C-axis table 42 is around the vertical axis 45 of the table, parallel to the Z-axis of the machine 10.
  • the C-axis table 42 has a center axis 45 and is mounted on a Y-axis table 48, and the Y-axis table is mounted on an X-axis table 50.
  • the X, Y, and Z-axis tables are servo driven, and are mounted on a base 52 that is supported on the floor.
  • the rotary table 42 is positioned at a convenient height relative to an operator 55, allowing for manual placement and removal of a tool 40 on the table 42 if desired.
  • the rotary table 42 may be placed at a height of less than six feet from the floor, and in one embodiment, the rotary table is placed at a height of no more than four feet from the floor.
  • An operator station including a control panel 56 for controlling the operation of the machine 10 may be provided next to the machine.
  • the head 24 is raised a small amount such as a few inches in order to allow a tool 40 to be placed on the rotary table 42.
  • the tool may be in the form of a film that is held in place by a vacuum that is applied by the table. The vacuum will hold the film in place during lamination, and will be turned off to allow the film and the laminate to be removed at the completion of the lamination.
  • the X, Y, and Z-axis tables are actuated to orient the tool relative to the head, and the head 24 is then lowered to place the compaction shoe or roller in contact with the tool 40. The head is then moved along the X-axis to pass the tool under the head in order to apply composite material to the tool in the desired pattern.
  • the relative motion between the head and the tool is achieved by movement of the tool relative to the head once the head is positioned at the correct level over the tool. Since the tool 40 is flat, movement of the head 24 in the vertical direction is not required during the composite material placement process. Conventional cutters (not shown) in the head 24 cut the composite material 15 as the head reaches the end of a course, and the head 24 may be raised a small amount by the linear actuator 36 or the internal compactor slide to allow the X, Y, and C-axis tables to reposition the tool 40 in order for the head to lay the next course.
  • the head 24 is then lowered to place the compaction roller or shoe 46 in contact with the tool 40, and the next course is laid by moving the tables that support the tool 40 relative to the head. Movement of the tool 40 to different positions in the X and Y-axes allows the stationary head 24 to apply composite material to different areas of the tool along the X and Y-axes. Rotation of the table around the C-axis allows the stationary head to apply composite material at various angles on the tool.
  • the device is used to produce small flat laminates.
  • the tool may be less than twenty-five square feet, or less than sixteen square feet, or less than ten square feet, or less than three square feet. Because the position of the head 24 is fixed relative to the creel 12 during application of fiber to the tool 40, the fiber delivery path length from the creel to the head is constant, and the path itself is simple and direct. Because the head 24 does not have to change its position during application of fiber to the head, a complicated wrist mechanism between the creel and the head is not needed.
  • the compact creel 12 and relatively simple table system for supporting the tool provides a complete fiber placement system with a small footprint.
  • the moving tables 42, 48, and 50 have a small mass compared to the normal moving parts of a fiber placement system, machine axes speeds and acceleration are high, and smaller motors than those used to maneuver a robot or gantry fiber placement system can be used for moving the tables relative to the head.

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  • Engineering & Computer Science (AREA)
  • Robotics (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
EP13158291.8A 2012-03-08 2013-03-08 System zur Platzierung von kleinem flachem Verbundwerkstoff Active EP2636516B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US201261608440P 2012-03-08 2012-03-08

Publications (2)

Publication Number Publication Date
EP2636516A1 true EP2636516A1 (de) 2013-09-11
EP2636516B1 EP2636516B1 (de) 2014-09-03

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Country Status (3)

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US (1) US8919410B2 (de)
EP (1) EP2636516B1 (de)
ES (1) ES2513017T3 (de)

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CN103640229A (zh) * 2013-12-30 2014-03-19 中国科学院自动化研究所 单驱动的复合材料铺丝头一体化装置
FR3044580A1 (fr) * 2015-12-08 2017-06-09 Coriolis Composites Machine d'application de fibres particuliere et procede de realisation de pieces mettant en oeuvre une telle machine
WO2017127276A1 (en) 2016-01-18 2017-07-27 Fives Machining Systems, Inc. Small 4-axis fiber placement machine
FR3141877A1 (fr) * 2022-11-15 2024-05-17 Coriolis Group Machine de placement de fibres

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Publication number Priority date Publication date Assignee Title
CN103640229A (zh) * 2013-12-30 2014-03-19 中国科学院自动化研究所 单驱动的复合材料铺丝头一体化装置
CN103640229B (zh) * 2013-12-30 2015-09-23 中国科学院自动化研究所 单驱动的复合材料铺丝头一体化装置
FR3044580A1 (fr) * 2015-12-08 2017-06-09 Coriolis Composites Machine d'application de fibres particuliere et procede de realisation de pieces mettant en oeuvre une telle machine
WO2017098093A1 (fr) * 2015-12-08 2017-06-15 Coriolis Composites Machine d'application de fibres particulières et procédé de réalisation de pièces mettant en œuvre une telle machine
WO2017127276A1 (en) 2016-01-18 2017-07-27 Fives Machining Systems, Inc. Small 4-axis fiber placement machine
EP3405331A4 (de) * 2016-01-18 2021-01-13 Fives Machining Systems, Inc. Kleine 4-achsige faserauflegemaschine
FR3141877A1 (fr) * 2022-11-15 2024-05-17 Coriolis Group Machine de placement de fibres
WO2024105310A1 (fr) * 2022-11-15 2024-05-23 Coriolis Group Machine et procédé de placement de fibres

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US8919410B2 (en) 2014-12-30
ES2513017T3 (es) 2014-10-24
EP2636516B1 (de) 2014-09-03
US20130233471A1 (en) 2013-09-12

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